EP0265546A1 - Machine with double acting box piston - Google Patents
Machine with double acting box piston Download PDFInfo
- Publication number
- EP0265546A1 EP0265546A1 EP86115059A EP86115059A EP0265546A1 EP 0265546 A1 EP0265546 A1 EP 0265546A1 EP 86115059 A EP86115059 A EP 86115059A EP 86115059 A EP86115059 A EP 86115059A EP 0265546 A1 EP0265546 A1 EP 0265546A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- head
- machine
- facing
- piston
- end interior
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/18—Other cylinders
- F02F1/183—Oval or square cylinders
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B7/00—Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
- F01B7/20—Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with two or more pistons reciprocating one within another, e.g. one piston forming cylinder of the other
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B9/00—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
- F01B9/02—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with crankshaft
- F01B9/023—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with crankshaft of Bourke-type or Scotch yoke
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/002—Double acting engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/32—Engines characterised by connections between pistons and main shafts and not specific to preceding main groups
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases or frames
- F02F7/0085—Materials for constructing engines or their parts
- F02F7/0087—Ceramic materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B1/00—Engines characterised by fuel-air mixture compression
- F02B1/02—Engines characterised by fuel-air mixture compression with positive ignition
- F02B1/04—Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
Definitions
- Reciprocating engines and pumps heretofore have been constructed with cylindrical pistons riding in fixed cylinder walls connected to a crankshaft by relatively long connecting rods. Due to the cylindrical nature of their construction and the space- taking connecting rods, none of these devices can provide a machine which can process a maximum amount of air for its size and weight and yet be efficient. It has heretofore been known that cube or box-shaped structures are very efficient for a given volume, but heretofore this principle has not been effectively employed in engine design. Also, prior art engines and pumps are mechanically stressed during operation to such an extent that ceramic or other heat resistant materials cannot be used successfully therewith. Therefore, they must be operated at relatively low temperatures which result in low thermal efficiencies.
- a machine which can be used as a two-cycle or a four-cycle diesel or gasoline engine or a pump.
- the double acting piston In its basic form, it employs two working chambers inside a double acting piston having a rectangular cross-section.
- the double acting piston In elevation, the double acting piston is generally box-shaped with opposite open sides.
- a stationary central block-shaped head is positioned within the piston and is connected to opposite stationary sidewalls which seal the opposite open sides thereof.
- the box-shaped piston is reciprocated by a crankshaft passing through and sliding transversely in a slot connected thereto usually adjacent one end thereof.
- the piston is supported for linear reciprocating movement against the sides of the case of the machine by suitable bearings.
- the head can include valves with suitable intake and exhaust ports, spark plugs, or fuel injectors when four-cycle machines are constructed.
- suitable bypass ports are provided about the head so that one working chamber on one side of the head acts as a pre-compression chamber and the other working chamber acts as a conventional two-cycle combustion chamber.
- a pair of box-shaped pistons can be included on opposite sides of the crankshaft so that four, four cycle working chambers can operate off of one throw of the crank or two, two cycle working chambers can operate off a single throw.
- the working chambers may be formed of walls which are non-planar and may be curved, etc. These walls may preferably be planar because planar walls can be supported against flexure, and the surfaces thereof can be treated with heat resistant material. This allows the machines to be run at much higher temperatures than is common for prior art engines and pumps so that radiant cooling becomes possible. This also makes the machines more thermodynamically efficient as large quantities of waste heat need not be extracted by a cooling system to maintain low operating temperatures; instead,more heat is converted into work within the machine.
- Another object is to provide a mechanical thermodynamic conversion device which can be constructed to operate at high temperatures.
- Another object is to provide a compact engine adapted to accommodate and withstand high pressures.
- number 20 in Figure 1 refers to a single piston two-cycle engine constructed according to the present invention.
- the engine 20 includes opposite side split case members 22 and 24 across which a crankshaft 26 extends to provide the power output of the engine 20.
- the case member 22 has an intake opening 21 for an intake manifold 28 which connects a suitable carburetor 30 to the engine 20 through a one way flapper valve 32 which prevents flow except from the carburetor 30 through the intake manifold 28 to the engine 20.
- the flapper valve 32 is shown for illustrative purposes only and may be replaced by any number of the known valves including those that are timed mechanically to the crankshaft 26.
- the case members 22 and 24 also include exhaust ports 34 and ignition means, such as the spark plug 36. The upper and lower portions of the case members 22 and 24 are held together by end covers 38 and 40.
- a central head block 44 is fixedly connected between the two case members 22 and 24 at a spaced location from the crankshaft 26.
- the case members 22 and 24 fixedly connected to and mating with two sides of the head block 44, the remaining head side 46, under head side 48, and sliding sides 50 and 52 are surrounded by a rectangular box-shaped piston 54 which is connected for movement to the arm 55 of the crankshaft 26 by means of a slot 56 formed in an extension 57 of the piston 54 and a pair of slider blocks 58 and 60.
- Rotation of the crankshaft 26 causes the piston 54 to move with respect to the head block 44 and the case sides 22 and 24 so that in the two-cycle machine described, one end surface 62 of the piston 54 acts as the top thereof while the opposite end surface 64 operates as its bottom.
- the sidewalls 66 and 68 of the piston 54 extend between the surfaces 62 and 64 act as the skirts of the piston 54 as well as portions of a pair of working chambers 70 and 72 which are defined within the piston 54 by the head block 44 and the case members 22 and 24.
- Seal strips 74 and 76 mounted midway in the sidewalls 66 and 68 of the piston 54 divide the two working chambers 70 and 72.
- Eight adjustable bearing pads 78 are included at the outer corners of the piston 54.
- the pads 78 adjust parallel to each other but are angled at about 15° and run on bearing strips 80 and 82 mounted on the case member 22 and bearing strips 84 and 86 mounted on the case member 24.
- the pads 78 are adjusted so that the piston 54 floats from the case members 22 and 24. This lack of contact allows high temperature materials such as ceramics to be used without fear that contact stresses will cause them to crack.
- Suitable materials for the pads 78 include hot pressed silicone nitride w hich can run unlubricated in most cases. It should be noted that the pads are not exposed to combustion and therefor run much cooler than the cylinder walls and pistons of conventional engines where the walls and pistons form the contacting bearing surfaces.
- the engine is in the midst of its exhaust and scavenging cycle. That is, exhaust 88 is flowing out of the ports 34 while a scavenging flow of air and fuel 89 in pre-compressed chamber 72 is flowing into working chamber 70 by means of a bypass 90 formed in the side 66 of the piston 54.
- the flow 89 is directed in the proper direction by a cutout 92 formed in the head side 46 of the head block 44 and shaped for that purpose.
- the piston 54 thereafter goes through top dead center, as shown in Figure 7, and the expansion of the burning gasses causes the piston 54 to move upwardly, as shown in Figure 8, the energy of the expansion being extracted out through the crankshaft 26 until the exhaust ports 34 are uncovered, whereupon the commencement of the flow of exhaust 88 out of the ports 34 commences.
- the positioning of the ports 34 is such that exhaust flow 88 commences prior to scavenging flow from the working chamber 72 wherein the air fuel mixture has been pre-compressed by the movement of the piston 54 upwardly. Thereafter, the engine 20 reaches the condition shown in Figure 3 and the cycle continues. If the working chambers 72 and 70 are disproportionate in size, that is, working chamber 72 being larger than working chamber 70, the engine 20 can be operated as two-stage air pump with energy being supplied thereto through the crankshaft 26.
- the piston 54 has opposite sides 94 and 96 which form sliding sealing surfaces adjacent the interior wall surfaces 98 and 100 of the case members 22 and 24, as shown in Figure 2.
- Seal strips 102 as shown with respect to side 94 in Figures 3 through 8, are embedded in the edges thereof to assure complete sealing by contact with the interior planar surfaces 98 and 100. Since this configuration is rectangular and does not expand or contract substantially in use, the seal strips 102 may be a solid rectangular seal or may be made up of various pieces. All usually are spring-loaded outwardly to assure good sealing contact.
- FIG. 9 is a diagrammatic cross-sectional view of a four-cycle, two piston, four working chamber engine 110 constructed according to the present invention.
- box shaped pistons 112 and 114 are connected to a crankshaft 116 by means of a slotted member 118 connected therebetween.
- the result is four working chambers, chambers 120, 122, 124 and 126.
- the working chambers 120 and 122 or 124 and 126, respectively are separated by head blocks 128 and 130.
- Each head block includes an intake port 132, an exhaust port 134, a pair of intake valves 136, a pair of exhaust valves 138 and suitable cam mechanisms 140 connected to the crankshaft 116 to drive the valves 136 and 138.
- the engine 110 is shown with the working chambers each part way through a different portion of the four-cycle.
- working chamber 120 is in its exhaust cycle while working chamber 122 is in the power cycle with both its in take and exhaust valves 136 and 138 closed.
- the working chamber 124 is in its compression cycle while working chamber 126 is in its intake cycle.
- Each of the working chambers cycle from intake to compression to power to exhaust, so that one working chamber is in the power cycle, one is in the exhaust, one is in the compression and one is in the intake, thus balancing the engine 110.
- the engine 110 can be operated as an air pump.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ceramic Engineering (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
The machine is an engine or pump with a box shaped piston (54) positioned between two stationary sidewalls (22,24). Opposite inward ends (62,64) and inwardly facing moving sidewalls (66,68) of the piston act with the two stationary case sidewalls (22,24) and a block-shaped central head (44) to define a pair of working chambers (70,72). The piston (54) moves as restrained by a crankshaft (26) to extract or add energy to the working chambers (70,72). Force is transferred between the piston (54) and the crankshaft (26) by means of a slide block (58) on the crankshaft (26) and the inner surfaces of a pair of parallel walls connected to the box shaped piston. Through the use of suitable cams (140) and valves (136,138), four-cycle, two-cylinder equivalent engines and two-cycle, one-cylinder equivalent engines can be produced per piston. The walls arangements of the machines maximize displacement while reducing mechanical stress and allowing use of heat resistant coating material, such as ceramics for thermal protection so that radiant cooling rather than separate fluid or gaseous cooling systems can be used.
Description
- Reciprocating engines and pumps heretofore have been constructed with cylindrical pistons riding in fixed cylinder walls connected to a crankshaft by relatively long connecting rods. Due to the cylindrical nature of their construction and the space- taking connecting rods, none of these devices can provide a machine which can process a maximum amount of air for its size and weight and yet be efficient. It has heretofore been known that cube or box-shaped structures are very efficient for a given volume, but heretofore this principle has not been effectively employed in engine design. Also, prior art engines and pumps are mechanically stressed during operation to such an extent that ceramic or other heat resistant materials cannot be used successfully therewith. Therefore, they must be operated at relatively low temperatures which result in low thermal efficiencies.
- A machine is provided which can be used as a two-cycle or a four-cycle diesel or gasoline engine or a pump. In its basic form, it employs two working chambers inside a double acting piston having a rectangular cross-section. In elevation, the double acting piston is generally box-shaped with opposite open sides. A stationary central block-shaped head is positioned within the piston and is connected to opposite stationary sidewalls which seal the opposite open sides thereof. The box-shaped piston is reciprocated by a crankshaft passing through and sliding transversely in a slot connected thereto usually adjacent one end thereof. The piston is supported for linear reciprocating movement against the sides of the case of the machine by suitable bearings. The head can include valves with suitable intake and exhaust ports, spark plugs, or fuel injectors when four-cycle machines are constructed. Otherwise, when two-cycle machines are constructed, suitable bypass ports are provided about the head so that one working chamber on one side of the head acts as a pre-compression chamber and the other working chamber acts as a conventional two-cycle combustion chamber. A pair of box-shaped pistons can be included on opposite sides of the crankshaft so that four, four cycle working chambers can operate off of one throw of the crank or two, two cycle working chambers can operate off a single throw.
- The working chambers may be formed of walls which are non-planar and may be curved, etc. These walls may preferably be planar because planar walls can be supported against flexure, and the surfaces thereof can be treated with heat resistant material. This allows the machines to be run at much higher temperatures than is common for prior art engines and pumps so that radiant cooling becomes possible. This also makes the machines more thermodynamically efficient as large quantities of waste heat need not be extracted by a cooling system to maintain low operating temperatures; instead,more heat is converted into work within the machine.
- It is therefore an object of the present invention to provide an engine or pump having rectangular combustion or compression cylinders which can accommodate most common engine cycles or operations.
- Another object is to provide a mechanical thermodynamic conversion device which can be constructed to operate at high temperatures.
- Another object is to provide a compact engine adapted to accommodate and withstand high pressures.
- These and other objects and advantages will become apparent to those skilled in the art after considering the following detailed specification and drawings wherein:
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- Figure 1 is a per spective view of an engine constructed according to the present invention;
- Figure 2 is an exploded perspective view of the engine of Figure 1;
- Figure 3 is a top cross-sectional view taken at line 3-3 of Figure 1;
- Figure 4 is an elevational cross-sectional view of the engine of Figures 1 through 3 in the equivalent of the bottom dead center position;
- Figure 5 is an elevational cross-sectional view of the engine of Figures 1 through 3 commencing its compression cycle;
- Figure 6 is an elevational cross-sectional view of the engine of Figures 1 through 3 at ignition;
- Figure 7 is an elevational cross-sectional view of the engine of Figures 1 through 3 in the equivalent of the top dead center position;
- Figure 8 is an elevational cross-sectional view of the engine of Figures 1 through 3 commencing its exhaust cycle; and
- Figure 9 is a diagrammatic side view of a four cylinder equivalent, twin piston, four-cycle machine constructed according to the present invention.
- Referring to the drawings more particularly by reference numbers,
number 20 in Figure 1 refers to a single piston two-cycle engine constructed according to the present invention. As shown, theengine 20 includes opposite sidesplit case members crankshaft 26 extends to provide the power output of theengine 20. Thecase member 22 has an intake opening 21 for anintake manifold 28 which connects a suitable carburetor 30 to theengine 20 through a oneway flapper valve 32 which prevents flow except from the carburetor 30 through theintake manifold 28 to theengine 20. Theflapper valve 32 is shown for illustrative purposes only and may be replaced by any number of the known valves including those that are timed mechanically to thecrankshaft 26. Thecase members exhaust ports 34 and ignition means, such as thespark plug 36. The upper and lower portions of thecase members - The basic configuration of the
engine 20 is more clearly seen from the views of Figures 2, 3 and 4. Acentral head block 44 is fixedly connected between the twocase members crankshaft 26. With thecase members head block 44, theremaining head side 46, underhead side 48, and slidingsides shaped piston 54 which is connected for movement to thearm 55 of thecrankshaft 26 by means of aslot 56 formed in anextension 57 of thepiston 54 and a pair ofslider blocks crankshaft 26 causes thepiston 54 to move with respect to thehead block 44 and thecase sides end surface 62 of thepiston 54 acts as the top thereof while theopposite end surface 64 operates as its bottom. Thesidewalls piston 54 extend between thesurfaces piston 54 as well as portions of a pair of workingchambers piston 54 by thehead block 44 and thecase members Seal strips sidewalls piston 54 divide the twoworking chambers adjustable bearing pads 78 are included at the outer corners of thepiston 54. Thepads 78 adjust parallel to each other but are angled at about 15° and run onbearing strips 80 and 82 mounted on thecase member 22 and bearingstrips 84 and 86 mounted on thecase member 24. Thepads 78 are adjusted so that thepiston 54 floats from thecase members pads 78 include hot pressed silicone nitride w hich can run unlubricated in most cases. It should be noted that the pads are not exposed to combustion and therefor run much cooler than the cylinder walls and pistons of conventional engines where the walls and pistons form the contacting bearing surfaces. - Looking at the operation of the
engine 20 in Figure 4, the engine is in the midst of its exhaust and scavenging cycle. That is,exhaust 88 is flowing out of theports 34 while a scavenging flow of air andfuel 89 inpre-compressed chamber 72 is flowing into workingchamber 70 by means of abypass 90 formed in theside 66 of thepiston 54. Theflow 89 is directed in the proper direction by acutout 92 formed in thehead side 46 of thehead block 44 and shaped for that purpose. - As the
crankshaft 26 turns it moves thepiston 54 downwardly until, as shown in Figure 5, both theexhaust ports 34 and thebypass 90 are closed so that the compression of thefuel air flow 89 can start to occur inworking chamber 70 while a partial vacuum is formed in workingchamber 72 drawing fuel and air thereinto from the carburetor 30 past theflapper valve 32. As shown in Figure 6, when thecrankshaft 26 has moved thepiston 54 close to what would normally be called top dead center, ignition occurs by means of thespark plug 36. Thepiston 54, thereafter goes through top dead center, as shown in Figure 7, and the expansion of the burning gasses causes thepiston 54 to move upwardly, as shown in Figure 8, the energy of the expansion being extracted out through thecrankshaft 26 until theexhaust ports 34 are uncovered, whereupon the commencement of the flow ofexhaust 88 out of theports 34 commences. It should be noted that the positioning of theports 34 is such thatexhaust flow 88 commences prior to scavenging flow from the workingchamber 72 wherein the air fuel mixture has been pre-compressed by the movement of thepiston 54 upwardly. Thereafter, theengine 20 reaches the condition shown in Figure 3 and the cycle continues. If the workingchambers chamber 72 being larger than workingchamber 70, theengine 20 can be operated as two-stage air pump with energy being supplied thereto through thecrankshaft 26. - In the configuration shown in Figures 1 through 8, the
piston 54 hasopposite sides interior wall surfaces case members Seal strips 102 as shown with respect toside 94 in Figures 3 through 8, are embedded in the edges thereof to assure complete sealing by contact with the interiorplanar surfaces seal strips 102 may be a solid rectangular seal or may be made up of various pieces. All usually are spring-loaded outwardly to assure good sealing contact. - Figure 9 is a diagrammatic cross-sectional view of a four-cycle, two piston, four working
chamber engine 110 constructed according to the present invention. In theengine 110, box shapedpistons member 118 connected therebetween. The result is four working chambers,chambers 120, 122, 124 and 126. In eachpiston chambers 120 and 122 or 124 and 126, respectively, are separated by head blocks 128 and 130. Each head block includes an intake port 132, anexhaust port 134, a pair of intake valves 136, a pair ofexhaust valves 138 andsuitable cam mechanisms 140 connected to the crankshaft 116 to drive thevalves 136 and 138. Theengine 110 is shown with the working chambers each part way through a different portion of the four-cycle. For example, since the exhaust valve into working chamber 120 is open and it is assumed that the crankshaft 116 is moving thepistons chamber 122 is in the power cycle with both its in take andexhaust valves 136 and 138 closed. The working chamber 124 is in its compression cycle while working chamber 126 is in its intake cycle. Each of the working chambers cycle from intake to compression to power to exhaust, so that one working chamber is in the power cycle, one is in the exhaust, one is in the compression and one is in the intake, thus balancing theengine 110. Of course, by properly valving the working chambers and providing power to the crankshaft, theengine 110 can be operated as an air pump. - Thus there have been shown and described novel engines and compressors which fulfill all of the objects and advantages sought therefor. Many changes, alterations, modifications and other uses and applications of the subject engines and compressors will become apparent to those skilled in the art after considering this specification together with the accompanying drawings and claims. All such changes, alterations and modifications which do not depart from the spirit and scope of the invention are deemed to be covered by the invention which is limited only by the claims which follow.
Claims (15)
1. A machine (20) having at least a first working chamber (70) formed by:
a machine case (22,24) with:
first and second stationary sidewall surfaces (98,100 resp. 22,24) facing each other; and
a first head surface (46) extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24);and
a first generally box shaped reciprocating piston (54, 112) having:
a first end interior surface (62) facing said first head surface (46); and
first and second reciprocating sidewall surfaces (66,68) extending between said first and second stationary sidewall surfaces (98,100 resp.22,24) and between said first end interior surface (62) and said first head surface (46) to define a first working chamber (70,112).
a machine case (22,24) with:
first and second stationary sidewall surfaces (98,100 resp. 22,24) facing each other; and
a first head surface (46) extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24);and
a first generally box shaped reciprocating piston (54, 112) having:
a first end interior surface (62) facing said first head surface (46); and
first and second reciprocating sidewall surfaces (66,68) extending between said first and second stationary sidewall surfaces (98,100 resp.22,24) and between said first end interior surface (62) and said first head surface (46) to define a first working chamber (70,112).
2. The machine defined in Claim 1 wherein said machine case further includes:
a first head block (44,128) on which said first head surface (46) is positioned, said first head block (44,128) being located within said first generally box shaped reciprocating piston (54,112) and having:
a second head surface (48) extending between said first and second stationary sidewall surfaces (98,100) formed thereon facing in an opposite direction from said first head surface (46), said first generally box shaped reciprocating piston (54,112) further including:
a second end interior surface (64) facing said second head surface (48) and toward said first end interior surface (62), said first and second reciprocating sidewall surfaces (66,68) extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24) and between said second end interior surface (64) and said second head surface (48) to define a second working chamber (72,122).
a first head block (44,128) on which said first head surface (46) is positioned, said first head block (44,128) being located within said first generally box shaped reciprocating piston (54,112) and having:
a second head surface (48) extending between said first and second stationary sidewall surfaces (98,100) formed thereon facing in an opposite direction from said first head surface (46), said first generally box shaped reciprocating piston (54,112) further including:
a second end interior surface (64) facing said second head surface (48) and toward said first end interior surface (62), said first and second reciprocating sidewall surfaces (66,68) extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24) and between said second end interior surface (64) and said second head surface (48) to define a second working chamber (72,122).
3. The machine defined in Claim 2 wherein said first generally box shaped reciprocating piston (54,112) further includes:
first and second parallel facing slide surfaces(62) positioned adjacent said first end interior surface thereof, said machine further including:
crankshaft means (26) supported by said machine case (22,24) and operatively connected for sliding contact to said piston (54) at said first and second parallel facing slide surfaces.
first and second parallel facing slide surfaces(62) positioned adjacent said first end interior surface thereof, said machine further including:
crankshaft means (26) supported by said machine case (22,24) and operatively connected for sliding contact to said piston (54) at said first and second parallel facing slide surfaces.
4. The machine defined in Claim 1 wherein said machine case further includes:
another first head surface extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24); and
another generally box shaped reciprocating piston (114) having:
another first end interior surface facing said other first head surface; and
another first and another second reciprocating sidewall surfaces extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24) and between said other first end interior surface and said other first head surface to define another first working chamber (124). (see Fig. 9)
another first head surface extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24); and
another generally box shaped reciprocating piston (114) having:
another first end interior surface facing said other first head surface; and
another first and another second reciprocating sidewall surfaces extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24) and between said other first end interior surface and said other first head surface to define another first working chamber (124). (see Fig. 9)
5. The machine defined in Claim 4 wherein said machine case further includes:
another head block (130) on which said other first head surface is positioned, said other head block (130) being located within said other generally box shaped reciprocating piston (114) and having:
another second surface extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24) formed thereon and facing in an opposite direction from said other first head surface, said other generally box shaped reciprocating piston (114) further including:
another first end interior surface facing said other second head surface and toward said other second end interior surface, said other first and other second reciprocating sidewall surfaces extending between said first and second stationary sidewall surfaces (98,100,resp. 22,24) and between said other second end interior surface and said other second head surface to define another second working chamber (126). (see Fig. 9)
another head block (130) on which said other first head surface is positioned, said other head block (130) being located within said other generally box shaped reciprocating piston (114) and having:
another second surface extending between said first and second stationary sidewall surfaces (98,100 resp. 22,24) formed thereon and facing in an opposite direction from said other first head surface, said other generally box shaped reciprocating piston (114) further including:
another first end interior surface facing said other second head surface and toward said other second end interior surface, said other first and other second reciprocating sidewall surfaces extending between said first and second stationary sidewall surfaces (98,100,resp. 22,24) and between said other second end interior surface and said other second head surface to define another second working chamber (126). (see Fig. 9)
6. The machine defined in Claim 5 wherein sa id other generally box shaped reciprocating piston (114) is connected to said one generally box shaped reciprocating piston (112) and further includes:
another first and second parallel facing slide surfaces positioned adjacent said other first end interior surface thereof. (see Fig. 9)
another first and second parallel facing slide surfaces positioned adjacent said other first end interior surface thereof. (see Fig. 9)
7. The machine defined in Claim 3 or 6 wherein said head block (44,128) includes:
check valve intake port means (28,32; 132,136), and said first stationary sidewall surface (22) includes:
exhaust port means (34,134) positioned to be opened and closed to said first working chamber (70,120) by said first end interior surface (62) moving therepast.
check valve intake port means (28,32; 132,136), and said first stationary sidewall surface (22) includes:
exhaust port means (34,134) positioned to be opened and closed to said first working chamber (70,120) by said first end interior surface (62) moving therepast.
8. The machine defined in Claim 3 or 6, wherein said first reciprocating sidewall surface (66) includes:
a transverse seal bearing (76) against said head block (44) to separate said first and second working chambers (70,72;120,122;124,126); and
a bypass passage (90) defined therein connected to said second working chamber (72), said head block first head surface (46) having:
a cutout (92) therein whereby said bypass passage (90) can communicate said first and second working chambers (70,72) when said generally box shaped reciprocating piston (54) is positioned with its first end interior surface (62) further from said first head surface (46) than said second end interior surface (64) is spaced from said second head surface (48).
a transverse seal bearing (76) against said head block (44) to separate said first and second working chambers (70,72;120,122;124,126); and
a bypass passage (90) defined therein connected to said second working chamber (72), said head block first head surface (46) having:
a cutout (92) therein whereby said bypass passage (90) can communicate said first and second working chambers (70,72) when said generally box shaped reciprocating piston (54) is positioned with its first end interior surface (62) further from said first head surface (46) than said second end interior surface (64) is spaced from said second head surface (48).
9. The machine defined in Claim 3 or 6 wherein said head block (e.g. 128) includes:
a first intake port (132);
a first exhaust port (134);
a first intake valve (136) positioned in said first intake port to control flow therethrough; and
a first exhaust valve (138) positioned in said first exhaust port to control flow therethrough. (see Fig.9)
a first intake port (132);
a first exhaust port (134);
a first intake valve (136) positioned in said first intake port to control flow therethrough; and
a first exhaust valve (138) positioned in said first exhaust port to control flow therethrough. (see Fig.9)
10. The machine defined in Claim 9 further including:
valve actuating means (140) connected between said crankshaft (116) and said first intake (136) and first exhaust valves (138) to actuate said valves in synchronism with rotation of said crankshaft (116).
valve actuating means (140) connected between said crankshaft (116) and said first intake (136) and first exhaust valves (138) to actuate said valves in synchronism with rotation of said crankshaft (116).
11. The machine defined in Claim 10 wherein said generally box shaped reciprocating piston (54; 128,130) includes:
first and second opposite rectangular side edges (94,96), said first opposite rectangular side edge (94) facing said first stationary sidewall surface (22,98) and said second opposite rectangular side edge (98) facing said second stationary sidewall surface (24,100) said first and second opposite rectangular side edges (94,96) each including:
seal means (102) which contact said first and second stationary sidewall surfaces (22,24) respectively to prevent flow thereabout.
first and second opposite rectangular side edges (94,96), said first opposite rectangular side edge (94) facing said first stationary sidewall surface (22,98) and said second opposite rectangular side edge (98) facing said second stationary sidewall surface (24,100) said first and second opposite rectangular side edges (94,96) each including:
seal means (102) which contact said first and second stationary sidewall surfaces (22,24) respectively to prevent flow thereabout.
12. The machine as defined in one of the claims 1 to 10 wherein said first and second stationary sidewall surfaces (22,24) each include:
a pair of bearing surfaces (80,82;84,86) thereon, and wherein said generally box shaped reciprocating piston (54,112) includes:
eight corners, each corner having:
an adjustable outwardly facing bearing pad (78) thereon positioned for engagement with one of said bearing surfaces (80,82;84,86);
first and second opposite rectangular side edges (94,96), said first opposite rectangular side edge (94) facing said first stationary sidewall surface (98) and being slightly spaced therefrom, and said second opposite rectangular side edge (96) facing said second stationary sidewall surface (100) and being slightly spaced therefrom, said first and second opposite rectangular side edges each including:
seal means (102) which contact said first and second stationary sidewall surfaces (98,100) respectively to prevent flow thereabout.
a pair of bearing surfaces (80,82;84,86) thereon, and wherein said generally box shaped reciprocating piston (54,112) includes:
eight corners, each corner having:
an adjustable outwardly facing bearing pad (78) thereon positioned for engagement with one of said bearing surfaces (80,82;84,86);
first and second opposite rectangular side edges (94,96), said first opposite rectangular side edge (94) facing said first stationary sidewall surface (98) and being slightly spaced therefrom, and said second opposite rectangular side edge (96) facing said second stationary sidewall surface (100) and being slightly spaced therefrom, said first and second opposite rectangular side edges each including:
seal means (102) which contact said first and second stationary sidewall surfaces (98,100) respectively to prevent flow thereabout.
13. The machine defined in Claim 12 wherein said adjustable outwardly facing bearing pads (78) are constructed from hot pressed silicon nitride.
14. The machine as defined in Claim 12 or 13 wherein said pair of bearing surfaces (80,82;84,86) on each of said first and second stationary sidewall surf aces (22,24) are each canted from parallel about 15°.
15. The machine defined in Claim 14 wherein said bearing pads (78) adjust inwardly and outwardly parallel to each other.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/667,416 US4625685A (en) | 1984-11-01 | 1984-11-01 | Machine with double acting box piston |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0265546A1 true EP0265546A1 (en) | 1988-05-04 |
Family
ID=24678123
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86115059A Withdrawn EP0265546A1 (en) | 1984-11-01 | 1986-10-30 | Machine with double acting box piston |
Country Status (2)
Country | Link |
---|---|
US (1) | US4625685A (en) |
EP (1) | EP0265546A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0454627A2 (en) * | 1990-02-26 | 1991-10-30 | Paolo Lombardi | Engine with double-acting pistons and without connecting rods |
WO2000060224A1 (en) * | 1999-04-06 | 2000-10-12 | Malcolm Leathwaite | The draw rotary engine |
CN104863706A (en) * | 2015-04-15 | 2015-08-26 | 丁健威 | Cylinder-driving two-stroke engine |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4625685A (en) * | 1984-11-01 | 1986-12-02 | Beshore Craig S | Machine with double acting box piston |
KR100461233B1 (en) * | 2001-12-03 | 2004-12-14 | 삼성광주전자 주식회사 | Apparatus for compressing fluid |
US7255071B2 (en) * | 2004-03-17 | 2007-08-14 | Beshore Craig S | Supercharged two-stroke engine with upper piston extensions |
US6966283B2 (en) * | 2004-03-17 | 2005-11-22 | Beshore Craig S | Apparatus with piston having upper piston extensions |
ITMI20110370A1 (en) * | 2011-03-10 | 2012-09-11 | Giorgio Amedeo Morandi | "PERFECTED INTERNAL COMBUSTION ENGINE" |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2067171A (en) * | 1933-01-24 | 1937-01-12 | Ralph H Beard | Engine |
DE680132C (en) * | 1936-01-23 | 1939-08-23 | Carl Axel Skaerlund | compressor |
US3910242A (en) * | 1974-07-25 | 1975-10-07 | Hawkins Hom | Internal combustion engine |
EP0119721A1 (en) * | 1983-02-28 | 1984-09-26 | Craig Spurgeon Beshore | Machine having integral piston and cylinder wall sections |
US4625685A (en) * | 1984-11-01 | 1986-12-02 | Beshore Craig S | Machine with double acting box piston |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1329514A (en) * | 1918-09-06 | 1920-02-03 | Dusoevoir Julius | Engine |
US2863426A (en) * | 1953-08-14 | 1958-12-09 | Summerlin Frederick Arthur | Internal combustion engines |
US3181516A (en) * | 1963-12-23 | 1965-05-04 | Ruben V Peterson | Internal combustion engine |
US4261303A (en) * | 1979-07-20 | 1981-04-14 | Ram-Z, Inc. | An internal combustion engine |
-
1984
- 1984-11-01 US US06/667,416 patent/US4625685A/en not_active Expired - Lifetime
-
1986
- 1986-10-30 EP EP86115059A patent/EP0265546A1/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2067171A (en) * | 1933-01-24 | 1937-01-12 | Ralph H Beard | Engine |
DE680132C (en) * | 1936-01-23 | 1939-08-23 | Carl Axel Skaerlund | compressor |
US3910242A (en) * | 1974-07-25 | 1975-10-07 | Hawkins Hom | Internal combustion engine |
EP0119721A1 (en) * | 1983-02-28 | 1984-09-26 | Craig Spurgeon Beshore | Machine having integral piston and cylinder wall sections |
US4625685A (en) * | 1984-11-01 | 1986-12-02 | Beshore Craig S | Machine with double acting box piston |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0454627A2 (en) * | 1990-02-26 | 1991-10-30 | Paolo Lombardi | Engine with double-acting pistons and without connecting rods |
EP0454627A3 (en) * | 1990-02-26 | 1992-12-16 | Paolo Lombardi | Engine with double-acting pistons and without connecting rods |
WO2000060224A1 (en) * | 1999-04-06 | 2000-10-12 | Malcolm Leathwaite | The draw rotary engine |
CN104863706A (en) * | 2015-04-15 | 2015-08-26 | 丁健威 | Cylinder-driving two-stroke engine |
Also Published As
Publication number | Publication date |
---|---|
US4625685A (en) | 1986-12-02 |
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